1) The document contains past year questions from GATE exams on the topic of Engineering Mechanics. It includes 30 multiple choice questions ranging from one to two marks.
2) The questions cover various concepts in mechanics including forces, moments, equilibrium, kinematics, collisions, friction etc. They involve calculations of tensions, velocities, accelerations, energies and powers for different mechanical systems.
3) Sample questions calculate reaction forces in trusses, velocities for particles and objects in motion, minimum forces required to move blocks etc. Diagrams are provided with the questions to illustrate the mechanical systems.
Deflection of structures using double integration method, moment area method, elastic load method, conjugate beam method, virtual work, castiglianois second theorem and method of consistent deformations
The document discusses the classification of structures based on stability and statical determinacy. It defines different types of supports and condition equations. A structure is stable and determinate if it has 3 reaction components that are neither parallel nor concurrent. It is stable but indeterminate if it has more than 3 non-parallel/concurrent reactions. Several examples of structures are classified. Structures with less than 3 reactions or with concurrent reactions are unstable. Closed panels require 3 internal condition equations to be stable internally.
Chapter 4-internal loadings developed in structural membersISET NABEUL
This document provides examples and explanations for determining internal forces like shear force and bending moment in structural members like beams and frames. It begins by introducing sign conventions and the procedure for analysis, which involves determining support reactions, drawing free body diagrams, and using equilibrium equations. Numerous step-by-step examples are then provided to demonstrate how to calculate and graph shear force and bending moment diagrams for beams and frames with different loading and support conditions.
This document contains fluid mechanics assignments from various years between 2003-2011 from the University of Newcastle in Australia. It includes multiple questions related to fluid flow, forces on objects, pressure and velocity calculations using concepts like continuity, momentum and energy equations. Head losses due to fittings are also discussed. Sample solutions are provided for some questions that involve calculations around gates, bends, contractions and other objects in fluid flow systems.
This document contains:
1) Instructions for a past IB exam paper that requires answering all questions from Section A and one from Section B within 75 minutes.
2) Three sample questions from Section A about physics concepts including motion in a magnetic field, forces on a rotating ball, and energy transfers.
3) Details for three optional questions in Section B, two involving multiple parts about topics in physics and one in chemistry.
Super-twisting sliding mode based nonlinear control for planar dual arm robotsjournalBEEI
This document describes a super-twisting sliding mode controller developed for a planar dual arm robot. The controller is designed to improve tracking ability and reduce chattering compared to a basic sliding mode controller. Mathematical models are developed to describe the kinematics and dynamics of the dual arm robot. A super-twisting algorithm is then applied within a sliding mode control framework to stabilize the robot and drive it to follow a desired trajectory. Simulations show the super-twisting controller has better tracking performance and less chattering than a conventional sliding mode controller.
4th 2 lecture shear and moment diagram structure imuhand mousa
This document discusses analyzing the internal loading of structural members by drawing shear force and bending moment diagrams for frames and beams. It provides examples of constructing shear force diagrams, bending moment diagrams, and normal force diagrams for different frame and beam configurations under various loading conditions using the method of superposition. It also assigns group works to draw the diagrams for additional frames and beams.
This document discusses the analysis of indeterminate beams using the moment distribution method. It provides the modified stiffness factor equation when the end of the beam is simply supported. It then gives an example problem and shows the step-by-step solution using the moment distribution method, including calculating the distribution factors, compiling the moment distribution table through multiple cycles, and determining the shear forces and bending moments. Finally, it briefly mentions analyzing nonprismatic members and using design tables with the moment distribution method.
Deflection of structures using double integration method, moment area method, elastic load method, conjugate beam method, virtual work, castiglianois second theorem and method of consistent deformations
The document discusses the classification of structures based on stability and statical determinacy. It defines different types of supports and condition equations. A structure is stable and determinate if it has 3 reaction components that are neither parallel nor concurrent. It is stable but indeterminate if it has more than 3 non-parallel/concurrent reactions. Several examples of structures are classified. Structures with less than 3 reactions or with concurrent reactions are unstable. Closed panels require 3 internal condition equations to be stable internally.
Chapter 4-internal loadings developed in structural membersISET NABEUL
This document provides examples and explanations for determining internal forces like shear force and bending moment in structural members like beams and frames. It begins by introducing sign conventions and the procedure for analysis, which involves determining support reactions, drawing free body diagrams, and using equilibrium equations. Numerous step-by-step examples are then provided to demonstrate how to calculate and graph shear force and bending moment diagrams for beams and frames with different loading and support conditions.
This document contains fluid mechanics assignments from various years between 2003-2011 from the University of Newcastle in Australia. It includes multiple questions related to fluid flow, forces on objects, pressure and velocity calculations using concepts like continuity, momentum and energy equations. Head losses due to fittings are also discussed. Sample solutions are provided for some questions that involve calculations around gates, bends, contractions and other objects in fluid flow systems.
This document contains:
1) Instructions for a past IB exam paper that requires answering all questions from Section A and one from Section B within 75 minutes.
2) Three sample questions from Section A about physics concepts including motion in a magnetic field, forces on a rotating ball, and energy transfers.
3) Details for three optional questions in Section B, two involving multiple parts about topics in physics and one in chemistry.
Super-twisting sliding mode based nonlinear control for planar dual arm robotsjournalBEEI
This document describes a super-twisting sliding mode controller developed for a planar dual arm robot. The controller is designed to improve tracking ability and reduce chattering compared to a basic sliding mode controller. Mathematical models are developed to describe the kinematics and dynamics of the dual arm robot. A super-twisting algorithm is then applied within a sliding mode control framework to stabilize the robot and drive it to follow a desired trajectory. Simulations show the super-twisting controller has better tracking performance and less chattering than a conventional sliding mode controller.
4th 2 lecture shear and moment diagram structure imuhand mousa
This document discusses analyzing the internal loading of structural members by drawing shear force and bending moment diagrams for frames and beams. It provides examples of constructing shear force diagrams, bending moment diagrams, and normal force diagrams for different frame and beam configurations under various loading conditions using the method of superposition. It also assigns group works to draw the diagrams for additional frames and beams.
This document discusses the analysis of indeterminate beams using the moment distribution method. It provides the modified stiffness factor equation when the end of the beam is simply supported. It then gives an example problem and shows the step-by-step solution using the moment distribution method, including calculating the distribution factors, compiling the moment distribution table through multiple cycles, and determining the shear forces and bending moments. Finally, it briefly mentions analyzing nonprismatic members and using design tables with the moment distribution method.
L15: Analysis of Indeterminate Beams by Slope Deflection Method Dr. OmPrakash
1) The document discusses analyzing indeterminate beams using the slope deflection method. It provides an example of determining moments at each joint of a frame.
2) Equilibrium equations are set up and solved simultaneously to find the slopes at specific joints.
3) The bending moment diagram is drawn based on the calculated slopes, with anticlockwise and clockwise moments indicated at each joint.
Dynamics of structures 5th edition chopra solutions manualSchneiderxds
Download at: https://goo.gl/bVUnH2
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This document discusses structural stability, statical determinacy, and influence lines. It defines stability as a prerequisite for structures to carry loads, which depends on comparing equations and unknown forces through structural analysis. Statical determinacy determines if a structure remains in equilibrium through static concepts alone. The number of external reactions must exceed the number of equilibrium equations. Influence lines show the variation of reactions, shear, or bending moment due to moving loads and identify their critical positions producing greatest effects.
This document presents a computational analysis of the structural components and behavior of flexible aircraft. It describes a MATLAB code used to determine natural frequencies and loads of a cantilever wing with stores in different spanwise positions. The code calculates natural frequencies from mass and stiffness matrices. Basis functions are used to represent bending and torsional modes. Validation shows computed torsion frequencies match experimental data, while bending frequencies have some offset. Parameters like store mass and position are investigated and found to affect natural frequencies.
This chapter discusses stress and strain in materials subjected to tension or compression. It defines stress as the load applied over the cross-sectional area. Strain is defined as the change in length over the original length. Hooke's law states that stress is proportional to strain for elastic materials. Young's modulus is the constant of proportionality between stress and strain. The chapter also discusses stress and strain calculations for materials with non-uniform cross-sections, as well as examples of stress and strain problems.
This document provides a preliminary design for a 20-story reinforced concrete building in Los Angeles. It outlines the design process, including establishing seismic loading based on ASCE 7-05 and distributing forces. A dual structural system of concrete shear walls and special moment frames is proposed. Preliminary sizing of structural elements is presented, along with calculations for seismic base shear, story shear distribution, and building overturning moment.
1. The document discusses electromagnetic concepts such as magnetic flux density, magnetic fields due to different current carrying conductors, and the torque experienced by a coil in a magnetic field.
2. Questions are provided about defining magnetic flux density, sketching magnetic field patterns, calculating torque on a coil, and ensuring the magnetic field is parallel to the coil plane.
3. Key concepts covered include magnetic fields, torque, magnetic flux density, and its SI unit of tesla.
Explains in detail about the planning and designing of a G + 2 school building both manually and using software (STAAD Pro).
With the reference with this we could design a building of a school with 2 blocks and G + 2 building.
Structural Analysis of a Bungalow Reportdouglasloon
Taylor's University Lakeside Campus
School of Architecture, Building & Design
Bachelor of Science (Hons) in Architecture
Building Structures (ARC 2523 / BLD 60103)
Project 2: Structural Analysis of a Bungalow
This document discusses two approximate methods for analyzing building frames subjected to loads: the portal method and cantilever method. The portal method assumes inflection points at midpoints of beams and mid-heights of columns, and that interior columns carry twice the shear of exterior columns. The cantilever method assumes inflection points at beam midpoints and column mid-heights, and that column axial stresses are proportional to their distance from the storey's centroid. Examples demonstrate applying each method to determine member forces in frames.
Compilation of questions on electromagnetism (questions only + ans for mcq)John Jon
1. A velocity selector is used to obtain an electron beam with a kinetic energy of 250 eV. Electrons with higher kinetic energies will pass through plate X, while electrons with lower kinetic energies will be deflected by plate Y.
2. When a current passes through a vertical wire PQ, a compass placed next to it may point in any of the four directions shown in the diagrams.
3. A uniform magnetic field applied in the same direction as an electric field maintaining a negatively charged plastic sphere at a constant height will have no effect on the sphere.
1) The document describes stress-strain diagrams from tensile tests on various materials including concrete, ceramics, steel, and alloys.
2) It provides data tables of load vs. strain measurements and asks the reader to plot stress-strain diagrams and determine values like modulus of elasticity, yield stress, and toughness.
3) Formulas are given for stress, strain, modulus of elasticity, and other mechanics of materials concepts as they relate to interpreting the stress-strain diagrams and tensile test data.
The document provides solutions to multiple mechanics of materials problems involving stress, strain, modulus of elasticity, yield strength, tensile strength, and ductility calculations for various materials like bronze, brass, and aluminum alloys. It includes determining maximum loads and deformations based on stress-strain curves, computing engineering and true stress-strain values, and using stress-strain data to find the true stress required for a given true plastic strain. Diagrams of stress-strain curves are generated from the data provided in the problems.
This document discusses structural analysis of cables and arches. It provides examples of determining tensions in cables subjected to concentrated and uniform loads. It also discusses the analysis procedure for cables under uniform loads. Examples are given for calculating tensions at different points of cables supporting bridges. Methods for analyzing fixed and hinged arches are demonstrated through examples finding internal forces at various arch sections.
This document contains a sample MCAT exam with 220 multiple choice questions covering physics, chemistry and biology. Some example questions are provided on topics like logic diagrams, stress-strain graphs, gas laws, radioactivity, optics and chemical reactions. The exam is designed for students completing their F.Sc. or non-F.Sc. degrees, with a maximum time of 150 minutes and total marks of 1100.
This document contains a question paper for an engineering mechanics examination with 15 multiple choice and numerical problems in two parts - Part A (10 short answer questions) and Part B (5 long answer questions). The questions cover topics in engineering mechanics including forces, moments, equilibrium, centroids, friction, kinematics and kinetics. Sample problems include determining tensions in cables for different structural configurations, calculating reaction forces and moments, finding centroids and moments of inertia for basic shapes, and solving problems involving projectile motion, motion on inclined planes, and minimum forces required to raise or move objects against friction. The document provides figures and diagrams to illustrate the systems described in several of the problems.
This document contains 40 multiple choice questions from previous GATE exams on the topic of electrical circuits and fields. The questions cover concepts such as circuit analysis, network theorems, capacitors, inductors, RLC circuits, and more. Sample questions test the calculation of current, voltage, power, impedance, and time constants in different circuit configurations.
This document contains a 50 question multiple choice exam on engineering mechanics topics like stress-strain behavior, bending of beams, torsion, columns, thermal stresses, and failure theories. The questions cover definitions, theories, and calculations related to properties of materials, stresses and strains, bending, shear, and combined stresses.
L15: Analysis of Indeterminate Beams by Slope Deflection Method Dr. OmPrakash
1) The document discusses analyzing indeterminate beams using the slope deflection method. It provides an example of determining moments at each joint of a frame.
2) Equilibrium equations are set up and solved simultaneously to find the slopes at specific joints.
3) The bending moment diagram is drawn based on the calculated slopes, with anticlockwise and clockwise moments indicated at each joint.
Dynamics of structures 5th edition chopra solutions manualSchneiderxds
Download at: https://goo.gl/bVUnH2
People also search:
dynamics of structures (5th edition) pdf
dynamics of structures chopra 5th edition pdf
dynamics of structures chopra 4th edition pdf
chopra dynamics of structures pdf
dynamics of structures theory and applications to earthquake engineering pdf
dynamics of structures anil k chopra
dynamics of structures chopra 3rd edition pdf
dynamics of structures: theory and applications to earthquake engineering 5th edition
This document discusses structural stability, statical determinacy, and influence lines. It defines stability as a prerequisite for structures to carry loads, which depends on comparing equations and unknown forces through structural analysis. Statical determinacy determines if a structure remains in equilibrium through static concepts alone. The number of external reactions must exceed the number of equilibrium equations. Influence lines show the variation of reactions, shear, or bending moment due to moving loads and identify their critical positions producing greatest effects.
This document presents a computational analysis of the structural components and behavior of flexible aircraft. It describes a MATLAB code used to determine natural frequencies and loads of a cantilever wing with stores in different spanwise positions. The code calculates natural frequencies from mass and stiffness matrices. Basis functions are used to represent bending and torsional modes. Validation shows computed torsion frequencies match experimental data, while bending frequencies have some offset. Parameters like store mass and position are investigated and found to affect natural frequencies.
This chapter discusses stress and strain in materials subjected to tension or compression. It defines stress as the load applied over the cross-sectional area. Strain is defined as the change in length over the original length. Hooke's law states that stress is proportional to strain for elastic materials. Young's modulus is the constant of proportionality between stress and strain. The chapter also discusses stress and strain calculations for materials with non-uniform cross-sections, as well as examples of stress and strain problems.
This document provides a preliminary design for a 20-story reinforced concrete building in Los Angeles. It outlines the design process, including establishing seismic loading based on ASCE 7-05 and distributing forces. A dual structural system of concrete shear walls and special moment frames is proposed. Preliminary sizing of structural elements is presented, along with calculations for seismic base shear, story shear distribution, and building overturning moment.
1. The document discusses electromagnetic concepts such as magnetic flux density, magnetic fields due to different current carrying conductors, and the torque experienced by a coil in a magnetic field.
2. Questions are provided about defining magnetic flux density, sketching magnetic field patterns, calculating torque on a coil, and ensuring the magnetic field is parallel to the coil plane.
3. Key concepts covered include magnetic fields, torque, magnetic flux density, and its SI unit of tesla.
Explains in detail about the planning and designing of a G + 2 school building both manually and using software (STAAD Pro).
With the reference with this we could design a building of a school with 2 blocks and G + 2 building.
Structural Analysis of a Bungalow Reportdouglasloon
Taylor's University Lakeside Campus
School of Architecture, Building & Design
Bachelor of Science (Hons) in Architecture
Building Structures (ARC 2523 / BLD 60103)
Project 2: Structural Analysis of a Bungalow
This document discusses two approximate methods for analyzing building frames subjected to loads: the portal method and cantilever method. The portal method assumes inflection points at midpoints of beams and mid-heights of columns, and that interior columns carry twice the shear of exterior columns. The cantilever method assumes inflection points at beam midpoints and column mid-heights, and that column axial stresses are proportional to their distance from the storey's centroid. Examples demonstrate applying each method to determine member forces in frames.
Compilation of questions on electromagnetism (questions only + ans for mcq)John Jon
1. A velocity selector is used to obtain an electron beam with a kinetic energy of 250 eV. Electrons with higher kinetic energies will pass through plate X, while electrons with lower kinetic energies will be deflected by plate Y.
2. When a current passes through a vertical wire PQ, a compass placed next to it may point in any of the four directions shown in the diagrams.
3. A uniform magnetic field applied in the same direction as an electric field maintaining a negatively charged plastic sphere at a constant height will have no effect on the sphere.
1) The document describes stress-strain diagrams from tensile tests on various materials including concrete, ceramics, steel, and alloys.
2) It provides data tables of load vs. strain measurements and asks the reader to plot stress-strain diagrams and determine values like modulus of elasticity, yield stress, and toughness.
3) Formulas are given for stress, strain, modulus of elasticity, and other mechanics of materials concepts as they relate to interpreting the stress-strain diagrams and tensile test data.
The document provides solutions to multiple mechanics of materials problems involving stress, strain, modulus of elasticity, yield strength, tensile strength, and ductility calculations for various materials like bronze, brass, and aluminum alloys. It includes determining maximum loads and deformations based on stress-strain curves, computing engineering and true stress-strain values, and using stress-strain data to find the true stress required for a given true plastic strain. Diagrams of stress-strain curves are generated from the data provided in the problems.
This document discusses structural analysis of cables and arches. It provides examples of determining tensions in cables subjected to concentrated and uniform loads. It also discusses the analysis procedure for cables under uniform loads. Examples are given for calculating tensions at different points of cables supporting bridges. Methods for analyzing fixed and hinged arches are demonstrated through examples finding internal forces at various arch sections.
This document contains a sample MCAT exam with 220 multiple choice questions covering physics, chemistry and biology. Some example questions are provided on topics like logic diagrams, stress-strain graphs, gas laws, radioactivity, optics and chemical reactions. The exam is designed for students completing their F.Sc. or non-F.Sc. degrees, with a maximum time of 150 minutes and total marks of 1100.
This document contains a question paper for an engineering mechanics examination with 15 multiple choice and numerical problems in two parts - Part A (10 short answer questions) and Part B (5 long answer questions). The questions cover topics in engineering mechanics including forces, moments, equilibrium, centroids, friction, kinematics and kinetics. Sample problems include determining tensions in cables for different structural configurations, calculating reaction forces and moments, finding centroids and moments of inertia for basic shapes, and solving problems involving projectile motion, motion on inclined planes, and minimum forces required to raise or move objects against friction. The document provides figures and diagrams to illustrate the systems described in several of the problems.
This document contains 40 multiple choice questions from previous GATE exams on the topic of electrical circuits and fields. The questions cover concepts such as circuit analysis, network theorems, capacitors, inductors, RLC circuits, and more. Sample questions test the calculation of current, voltage, power, impedance, and time constants in different circuit configurations.
This document contains a 50 question multiple choice exam on engineering mechanics topics like stress-strain behavior, bending of beams, torsion, columns, thermal stresses, and failure theories. The questions cover definitions, theories, and calculations related to properties of materials, stresses and strains, bending, shear, and combined stresses.
This document contains 25 multiple choice questions from a GATE exam for Electrical Engineering in 2011. The questions cover topics in circuits, signals and systems, control systems, power systems, electronics, and digital logic. The document is presented as a practice test to help students prepare for the GATE EE exam.
This document contains a 20 question multiple choice quiz related to engineering topics. Some of the questions are about matrices, probability, thermodynamics, fluid mechanics, heat transfer, and mechanics of materials. The correct answers are provided for reference.
This document contains 30 multiple choice questions from a GATE EE exam, along with explanations for the answers. It discusses topics related to electrical engineering, including circuits, electromagnetism, power systems, and electrical machines. The questions range from basic circuit analysis and energy calculations to more complex topics involving synchronous generators, induction motors, and HVDC transmission systems. The document is intended as a practice resource for the GATE EE exam.
This document appears to be a sample test for the MCAT exam containing 220 multiple choice questions testing physics and chemistry knowledge. The physics section includes questions about electric fields, forces, fluids, waves, optics, mechanics, and magnetism. The chemistry section includes questions about polymers, gases, atomic structure, bonding, thermodynamics, and organic chemistry. The document provides context for understanding the content and scope of the MCAT exam for students in a medical program entrance test.
This document contains a sample MCAT exam with 220 multiple choice questions covering physics, chemistry and biology. The physics section includes questions about magnetic fields, vectors, projectile motion, waves, optics and electricity & magnetism. The chemistry section tests concepts such as stoichiometry, gas laws, thermodynamics, electrochemistry and organic chemistry. The biology portion covers topics like cell structure, genetics, evolution and human physiology.
The document discusses composite beams, which combine steel beams with concrete slabs to act compositely. It provides examples and discusses the advantages of composite beams over normal steel beams. The performance of composite beams is similar to reinforced concrete beams, but differs in that the steel beam's properties cannot be ignored and shear connection is needed between the steel and concrete. Design of composite beams follows reinforced concrete design methods with modifications. An example problem is provided to demonstrate the design process for a composite beam, including checking the beam properties, shear connectors, and deflection.
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Top mailing list providers in the USA.pptxJeremyPeirce1
Discover the top mailing list providers in the USA, offering targeted lists, segmentation, and analytics to optimize your marketing campaigns and drive engagement.
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This presentation is a curated compilation of PowerPoint diagrams and templates designed to illustrate 20 different digital transformation frameworks and models. These frameworks are based on recent industry trends and best practices, ensuring that the content remains relevant and up-to-date.
Key highlights include Microsoft's Digital Transformation Framework, which focuses on driving innovation and efficiency, and McKinsey's Ten Guiding Principles, which provide strategic insights for successful digital transformation. Additionally, Forrester's framework emphasizes enhancing customer experiences and modernizing IT infrastructure, while IDC's MaturityScape helps assess and develop organizational digital maturity. MIT's framework explores cutting-edge strategies for achieving digital success.
These materials are perfect for enhancing your business or classroom presentations, offering visual aids to supplement your insights. Please note that while comprehensive, these slides are intended as supplementary resources and may not be complete for standalone instructional purposes.
Frameworks/Models included:
Microsoft’s Digital Transformation Framework
McKinsey’s Ten Guiding Principles of Digital Transformation
Forrester’s Digital Transformation Framework
IDC’s Digital Transformation MaturityScape
MIT’s Digital Transformation Framework
Gartner’s Digital Transformation Framework
Accenture’s Digital Strategy & Enterprise Frameworks
Deloitte’s Digital Industrial Transformation Framework
Capgemini’s Digital Transformation Framework
PwC’s Digital Transformation Framework
Cisco’s Digital Transformation Framework
Cognizant’s Digital Transformation Framework
DXC Technology’s Digital Transformation Framework
The BCG Strategy Palette
McKinsey’s Digital Transformation Framework
Digital Transformation Compass
Four Levels of Digital Maturity
Design Thinking Framework
Business Model Canvas
Customer Journey Map
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How MJ Global Leads the Packaging Industry.pdfMJ Global
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This PowerPoint compilation offers a comprehensive overview of 20 leading innovation management frameworks and methodologies, selected for their broad applicability across various industries and organizational contexts. These frameworks are valuable resources for a wide range of users, including business professionals, educators, and consultants.
Each framework is presented with visually engaging diagrams and templates, ensuring the content is both informative and appealing. While this compilation is thorough, please note that the slides are intended as supplementary resources and may not be sufficient for standalone instructional purposes.
This compilation is ideal for anyone looking to enhance their understanding of innovation management and drive meaningful change within their organization. Whether you aim to improve product development processes, enhance customer experiences, or drive digital transformation, these frameworks offer valuable insights and tools to help you achieve your goals.
INCLUDED FRAMEWORKS/MODELS:
1. Stanford’s Design Thinking
2. IDEO’s Human-Centered Design
3. Strategyzer’s Business Model Innovation
4. Lean Startup Methodology
5. Agile Innovation Framework
6. Doblin’s Ten Types of Innovation
7. McKinsey’s Three Horizons of Growth
8. Customer Journey Map
9. Christensen’s Disruptive Innovation Theory
10. Blue Ocean Strategy
11. Strategyn’s Jobs-To-Be-Done (JTBD) Framework with Job Map
12. Design Sprint Framework
13. The Double Diamond
14. Lean Six Sigma DMAIC
15. TRIZ Problem-Solving Framework
16. Edward de Bono’s Six Thinking Hats
17. Stage-Gate Model
18. Toyota’s Six Steps of Kaizen
19. Microsoft’s Digital Transformation Framework
20. Design for Six Sigma (DFSS)
To download this presentation, visit:
https://www.oeconsulting.com.sg/training-presentations
Innovation Management Frameworks: Your Guide to Creativity & Innovation
Engineering Mechanics.pdf
1. CHAPTER 2
ENGINEERING MECHANICS
GATE Previous Year Solved Paper For Mechanical Engineering
Published by: NODIA and COMPANY ISBN: 9788192276250
Visit us at: www.nodia.co.in
YEAR 2012 TWO MARKS
Common Data For Q.
• 1 and 2
Two steel truss members, and
AC BC , each having cross sectional area of
100 mm2
, are subjected to a horizontal force F as shown in figure. All the
joints are hinged.
MCQ 2.1 If 1 kN
F = , the magnitude of the vertical reaction force developed at the
point B in kN is
(A) 0.63 (B) 0.32
(C) 1.26 (D) 1.46
MCQ 2.2 The maximum force F is kN that can be applied at C such that the axial
stress in any of the truss members DOES NOT exceed 100 MPa is
(A) 8.17 (B) 11.15
(C) 14.14 (D) 22.30
YEAR 2011 ONE MARK
MCQ 2.3 The coefficient of restitution of a perfectly plastic impact is
(A) 0 (B) 1
(C) 2 (D) 3
MCQ 2.4 A stone with mass of 0.1 kg is catapulted as shown in the figure. The total
force Fx (in N) exerted by the rubber band as a function of distance x
2. PAGE 72 ENGINEERING MECHANICS CHAP 2
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(in m) is given by F x
300
x
2
= . If the stone is displaced by 0.1 m from the
un-stretched position ( )
x 0
= of the rubber band, the energy stored in the
rubber band is
(A) 0.01 J (B) 0.1 J
(C) 1 J (D) 10 J
YEAR 2011 TWO MARKS
MCQ 2.5 A 1 kg block is resting on a surface with coefficient of friction 0.1
μ = . A
force of 0.8 N is applied to the block as shown in the figure. The friction
force is
(A) 0 (B) 0.8 N
(C) 0.98 N (D) 1.2 N
YEAR 2009 ONE MARK
MCQ 2.6 A block weighing 981 N is resting on a horizontal surface. The coefficient of
friction between the block and the horizontal surface is 0.2
μ = . A vertical
cable attached to the block provides partial support as shown. A man can
pull horizontally with a force of 100 N. What will be the tension, T (in N)
in the cable if the man is just able to move the block to the right ?
(A) 176.2 (B) 196.0
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(C) 481.0 (D) 981.0
YEAR 2009 TWO MARKS
MCQ 2.7 A uniform rigid rod of mass M and length L is hinged at one end as shown
in the adjacent figure. A force P is applied at a distance of /
L
2 3 from the
hinge so that the rod swings to the right. The reaction at the hinge is
(A) P
− (B) 0
(C) /
P 3 (D) /
P
2 3
YEAR 2008 ONE MARK
MCQ 2.8 A straight rod length ( )
L t , hinged at one end freely extensible at the other
end, rotates through an angle ( )
t
θ about the hinge. At time t, ( ) 1
L t =
m, ( ) 1
L t =
o m/s, ( )
t
4
θ π
= rad and ( ) 1
t
θ =
o rad/s. The magnitude of the
velocity at the other end of the rod is
(A) 1 m/s (B) 2 m/s
(C) 3 m/s (D) 2 m/s
YEAR 2008 TWO MARKS
MCQ 2.9 A circular disk of radius R rolls without slipping at a velocity V . The
magnitude of the velocity at point P (see figure) is
4. PAGE 74 ENGINEERING MECHANICS CHAP 2
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(A) V
3 (B) /2
V
3
(C) /2
V (D) 2 /
V 3
MCQ 2.10 Consider a truss PQR loaded at P with a force F as shown in the figure -
The tension in the member QR is
(A) 0.5 F (B) 0.63 F
(C) 0.73 F (D) 0.87 F
YEAR 2007 ONE MARK
MCQ 2.11 During inelastic collision of two particles, which one of the following is
conserved ?
(A) Total linear momentum only
(B) Total kinetic energy only
(C) Both linear momentum and kinetic energy
(D) Neither linear momentum nor kinetic energy
YEAR 2007 TWO MARKS
MCQ 2.12 A block of mass M is released from point P on a rough inclined plane with
inclination angle θ, shown in the figure below. The co-efficient of friction is
μ. If tan
<
μ θ, then the time taken by the block to reach another point Q
on the inclined plane, where PQ s
= , is
(A)
( )
cos tan
g
s
2
θ θ μ
−
(B)
( )
cos tan
g
s
2
θ θ μ
+
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(C)
( )
sin tan
g
s
2
θ θ μ
−
(D)
( )
sin tan
g
s
2
θ θ μ
+
YEAR 2006 TWO MARKS
MCQ 2.13 If a system is in equilibrium and the position of the system depends upon
many independent variables, the principles of virtual work states that the
partial derivatives of its total potential energy with respect to each of the
independent variable must be
(A) 1.0
− (B) 0
(C) 1.0 (D) 3
MCQ 2.14 If point A is in equilibrium under the action of the applied forces, the values
of tensions TAB and TAC are respectively
(A) 520 N and 300 N (B) 300 N and 520 N
(C) 450 N and 150 N (D) 150 N and 450 N
YEAR 2005 ONE MARK
MCQ 2.15 The time variation of the position of a particle in rectilinear motion is given
by 2 2
x t t t
3 2
= + + . If v is the velocity and a is the acceleration of the
particle in consistent units, the motion started with
(A) 0, 0
v a
= = (B) 0, 2
v a
= =
(C) 2, 0
v a
= = (D) 2, 2
v a
= =
MCQ 2.16 A simple pendulum of length of 5 m, with a bob of mass 1 kg, is in simple
harmonic motion. As it passes through its mean position, the bob has a
speed of 5 m/s. The net force on the bob at the mean position is
(A) zero (B) 2.5 N
(C) 5 N (D) 25 N
YEAR 2005 TWO MARKS
MCQ 2.17 Two books of mass 1 kg each are kept on a table, one over the other. The
6. PAGE 76 ENGINEERING MECHANICS CHAP 2
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coefficient of friction on every pair of contacting surfaces is 0.3. The lower
book is pulled with a horizontal force F . The minimum value of F for which
slip occurs between the two books is
(A) zero (B) 1.06 N
(C) 5.74 N (D) 8.83 N
MCQ 2.18 A shell is fired from a cannon. At the instant the shell is just about to leave
the barrel, its velocity relative to the barrel is 3 m/s, while the barrel is
swinging upwards with a constant angular velocity of 2 rad/s. The magnitude
of the absolute velocity of the shell is
(A) 3 m/s (B) 4 m/s
(C) 5 m/s (D) 7 m/s
MCQ 2.19 An elevator (lift) consists of the elevator cage and a counter weight, of mass
m each. The cage and the counterweight are connected by chain that passes
over a pulley. The pulley is coupled to a motor. It is desired that the elevator
should have a maximum stopping time of t seconds from a peak speed v. If
the inertias of the pulley and the chain are neglected, the minimum power
that the motor must have is
(A) mV
2
1 2
(B)
t
mV
2
2
(C)
t
mV2
(D)
t
mV
2 2
MCQ 2.20 A 1 kg mass of clay, moving with a velocity of 10 m/s, strikes a stationary
wheel and sticks to it. The solid wheel has a mass of 20 kg and a radius of
7. CHAP 2 ENGINEERING MECHANICS PAGE 77
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1 m. Assuming that the wheel is set into pure rolling motion, the angular
velocity of the wheel immediately after the impact is approximately
(A) zero (B)
3
1 rad/s
(C)
3
10 rad/s (D)
3
10 rad/s
YEAR 2004 ONE MARK
MCQ 2.21 The figure shows a pin-jointed plane truss loaded at the point M by hanging
a mass of 100 kg. The member LN of the truss is subjected to a load of
(A) 0 Newton (B) 490 Newtons in compression
(C) 981 Newtons in compression (D) 981 Newtons in tension
YEAR 2004 TWO MARKS
MCQ 2.22 An ejector mechanism consists of a helical compression spring having a
spring constant of 981 10
k N/m
3
#
= . It is pre-compressed by 100 mm from
its free state. If it is used to eject a mass of 100 kg held on it, the mass will
move up through a distance of
8. PAGE 78 ENGINEERING MECHANICS CHAP 2
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(A) 100 mm (B) 500 mm
(C) 581 mm (D) 1000 mm
MCQ 2.23 A rigid body shown in the figure (a) has a mass of 10 kg. It rotates with
a uniform angular velocity ‘ω’. A balancing mass of 20 kg is attached as
shown in figure (b). The percentage increase in mass moment of inertia as a
result of this addition is
(A) 25% (B) 50%
(C) 100% (D) 200%
MCQ 2.24 The figure shows a pair of pin-jointed gripper-tongs holding an object
weighting 2000 N. The coefficient of friction (μ) at the gripping surface
is 0.1 XX is the line of action of the input force and YY is the line of
application of gripping force. If the pin-joint is assumed to be frictionless,
the magnitude of force F required to hold the weight is
(A) 1000 N (B) 2000 N
(C) 2500 N (D) 5000 N
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YEAR 2003 ONE MARK
MCQ 2.25 A truss consists of horizontal members (AC,CD, DB and EF) and vertical
members (CE and DF) having length l each. The members AE, DE and BF
are inclined at 45c to the horizontal. For the uniformly distributed load “p”
per unit length on the member EF of the truss shown in figure given below,
the force in the member CD is
(A)
pl
2
(B) pl
(C) 0 (D)
pl
3
2
MCQ 2.26 A bullet of mass “m” travels at a very high velocity v (as shown in the
figure) and gets embedded inside the block of mass “M ” initially at rest on
a rough horizontal floor. The block with the bullet is seen to move a distance
“s” along the floor. Assuming μ to be the coefficient of kinetic friction
between the block and the floor and “g” the acceleration due to gravity
what is the velocity v of the bullet ?
(A)
m
M m gs
2μ
+ (B)
m
M m gs
2μ
−
(C)
( )
m
M m
gs
2
μ
μ
+
(D)
m
M gs
2μ
YEAR 2003 TWO MARKS
Common Data For Q.
• Data for Q. 27 & 28 are given below. Solve
the problems and choose correct answers.
A reel of mass “m” and radius of gyration “k” is rolling down smoothly from
rest with one end of the thread wound on it held in the ceiling as depicated
in the figure. Consider the thickness of thread and its mass negligible in
comparison with the radius “r ” of the hub and the reel mass “m”. Symbol
“g” represents the acceleration due to gravity.
10. PAGE 80 ENGINEERING MECHANICS CHAP 2
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MCQ 2.27 The linear acceleration of the reel is
(A)
( )
r k
gr
2 2
2
+
(B)
( )
r k
gk
2 2
2
+
(C)
( )
r k
grk
2 2
+
(D)
( )
r k
mgr
2 2
2
+
MCQ 2.28 The tension in the thread is
(A)
( )
r k
mgr
2 2
2
+
(B)
( )
r k
mgrk
2 2
+
(C)
( )
r k
mgk
2 2
2
+
(D)
( )
r k
mg
2 2
+
YEAR 2001 ONE MARK
MCQ 2.29 A particle P is projected from the earth surface at latitude 45c with escape
velocity 11.19 /
km s
v = . The velocity direction makes an angle α with the
local vertical. The particle will escape the earth’s gravitational field
(A) only when 0
α = (B) only when 45c
α =
(C) only when 90c
α = (D) irrespective of the value of α
MCQ 2.30 The area moment of inertia of a square of size 1 unit about its diagonal is
(A)
3
1 (B)
4
1
(C)
12
1 (D)
6
1
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YEAR 2001 TWO MARKS
MCQ 2.31 For the loading on truss shown in the figure, the force in member CD is
(A) zero (B) 1 kN
(C) kN
2 (D)
2
kN
1
MCQ 2.32 Bodies 1 and 2 shown in the figure have equal mass m. All surfaces are
smooth. The value of force P required to prevent sliding of body 2 on body
1 is
(A) 2 mg
P = (B) mg
P 2
=
(C) 2 mg
P 2
= (D) P mg
=
MCQ 2.33 Mass M slides in a frictionless slot in the horizontal direction and the bob
of mass m is hinged to mass M at C , through a rigid massless rod. This
system is released from rest with 30c
θ = . At the instant when 0c
θ = , the
velocities of m and M can be determined using the fact that, for the system
(i.e., m and M together)
12. PAGE 82 ENGINEERING MECHANICS CHAP 2
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(A) the linear momentum in x and y directions are conserved but the energy
is not conserved.
(B) the linear momentum in x and y directions are conserved and the energy
is also conserved.
(C) the linear momentum in x direction is conserved and the energy is also
conserved.
(D) the linear momentum in y direction is conserved and the energy is also
conserved.
*********
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SOLUTION
SOL 2.1 Option (A) is correct.
From above figure. Three forces are acting on a common point. Hence by
Lami’s Theorem.
( )
sin
F
105c sin sin
T T
120 135
2 1
c c
= =
&
sin
T
135
1
c sin sin
F
105 105
1
c c
= =
T1 0.7320 kN
=
Hence vertical reaction at B,
RNT1
cos
T 30
1 c
= . cos
0 73205 30
# c
= 0.634 kN
=
SOL 2.2 Option (B) is correct.
From Previous question
sin
F
105c sin
T
120
2
c
=
T2 .
sin
sin F F
135
120 0 8965
#
c
= =
and T1 ( . )F
0 73205
=
T2 T
> 1
σ 100 MPa
= (given)
As we know F A1
σ #
=
& Fmax A
max 1
σ #
=
T2 100 100
#
=
. F
0 8965 100 100
#
=
F
.
11154.5 N
0 8965
100 100
#
= = 11.15 kN
=
14. PAGE 84 ENGINEERING MECHANICS CHAP 2
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SOL 2.3 Option (A) is correct.
From the Newton’s Law of collision of Elastic bodies.
Velocity of separation e #
= Velocity of approach
( )
V V
2 1
− ( )
e U U
1 2
= −
Where e is a constant of proportionality & it is called the coefficient of
restitution and its value lies between 0 to 1. The coefficient of restitution
of a perfectly plastic impact is zero, because all the K.E. will be absorbed
during perfectly plastic impact.
SOL 2.4 Option (B) is correct.
Given : Fx x
300 2
= , Position of x is, x 0
= to .
x 0 1
=
The energy stored in the rubber band is equal to work done by the stone.
Hence dE F dx
x
=
Integrating both the sides & put the value of F & limits
dE
E
0
# x dx
300
.
2
0
0 1
= #
E x
300
3
.
3
0
0 1
= : D 300
( . )
0.1 Joule
3
0 1 3
= =
; E
SOL 2.5 Option (B) is correct.
Given : 1 kg
m = , μ .
0 1
= ; From FBD : RN mg
=
Now static friction force,
fS R mg
N
μ μ
= = 0.1 1 9.8 0.98 N
# #
= =
Applied force F 0.8 N
= is less then, the static friction 0.98 N
fS =
F f
< S
So, we can say that the friction developed will equal to the applied force
F 0.8 N
=
SOL 2.6 Option (C) is correct.
Given : 981 N
W = , 0.2
μ =
First of all we have to make a FBD of the block
Here, RN = Normal reaction force
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T =Tension in string
Using the balancing of forces, we have
0
Fx
Σ = : RN
μ 100 N
=
RN
.
500 N
100
0 2
100
μ
= = =
and 0
Fy
Σ = or downward forces = upward forces
W T RN
= + & T W RN
= − 981 500 48 N
1
= − =
SOL 2.7 Option (B) is correct.
When rod swings to the right, linear acceleration a and angular acceleration
α comes in action. Centre of gravity (G) acting at the mid-point of the rod.
Let R be the reaction at the hinge.
Linear acceleration a .
r α
= L
2 # α
=
L
a
2
= ...(i)
and about point G, for rotational motion
G
Μ
/ IG # α
=
R L P L
2 6
+
b b
l l
ML
L
a
12
2
2
= b l From equation (i)
R P
3
+ Ma
3
=
a
M
R
M
P
3
= + ...(ii)
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By equilibrium of forces in normal direction to the rod
Fm
/ 0
= : P R
− Ma
= M
M
R
M
P
3
= +
b l From equation (ii)
P R
− R P
3
= +
& R 0
= So, reaction at the hinge is zero.
SOL 2.8 Option (D) is correct.
Let : Vt =Tangential Velocity
Vr =Relative Velocity
V =Resultant Velocity
Let rod of length ( )
L t increases by an amount ( )
L t
T .
Given ( )
L t 1
= m, ( )
L t
:
=1 m/sec, ( )
t
4
θ π
= rad, ( )
t
θ
:
=1 rad/sec
Time taken by the rod to turn
4
π rad is,
t
( )
( )
tan
velocity
dis ce
t
t
θ
θ
= = :
/
1
4
4
π π
= = sec
So, increase in length of the rod during this time will be
( )
L t
Δ ( )
L t t
#
=
4
1
4
#
π π
= = meter
Rod turn
4
π radian. So, increased length after
4
π sec, (New length)
.
1
4
1 785
π
= + =
a k m
Now, tangential velocity,
Vt .
R ω
= . .
1 785 1 1 785
#
= = m/sec ( )
t
ω θ
= o
Radial velocity, Vr ( )
L t
=
:
=1 m/sec
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Therefore, the resultant velocity will be
VR V V
t r
2 2
= + ( . ) ( ) 2.04 2 /sec
m
1 785 1
2 2
-
= + =
SOL 2.9 Option (A) is correct.
When disc rolling along a straight path, without slipping. The centre of the
wheel O moves with some linear velocity and each particle on the wheel
rotates with some angular velocity.
Thus, the motion of any particular on the periphery of the wheel is a
combination of linear and angular velocity.
Let wheel rotates with angular velocity=ω rad/sec.
So, ω
R
V
= ....(i)
Velocity at point P is, VP PQ
#
ω
= ...(ii)
From triangle OPQ PQ ( ) ( ) 2 ( )
cos
OQ OP OQ OP POQ
2 2
+
# #
+ −
( ) ( ) 2 120
cos
R R RR
2 2
c
= + −
( ) ( ) ( )
R R R
2 2 2
= + + R
3
= ...(iii)
From equation (i), (ii) and (iii)
VP
R
V R
3
#
= V
3
=
SOL 2.10 Option (B) is correct.
The forces which are acting on the truss PQR is shown in figure.
We draw a perpendicular from the point P, that intersects QR at point S .
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Let PS QS a
= =
RQ & RR are the reactions acting at point Q & R respectively.
Now from the triangle PRS
tan30c
SR
PS
= & SR 1.73
tan
PS a a a
30
3
3
1
c
= = = =
Taking the moment about point R,
( . )
R a a
1 73
Q # + .
F a
1 73
#
=
RQ
.
.
.
. .
F F F
a
a
2 73
1 73
2 73
1 73 0 634
= = =
From equilibrium of the forces, we have
R R
R Q
+ F
=
RR 0.634 F
F R F
Q
= − = − 0.366 F
=
To find tension in QR we have to use the method of joint at point Q, and
F 0
y
Σ =
sin
F 45
QP c RQ
=
FQP
0.634 0.8966
F F
2
1
= =
and, 0
Fx
Σ =
cos
F 45
QP c FQR
= & FQR 0.8966 0.634 0.63
F F F
2
1 -
#
= =
SOL 2.11 Option (A) is correct.
In both elastic & in inelastic collision total linear momentum remains
conserved. In the inelastic collision loss in kinetic energy occurs because the
coefficient of restitution is less than one and loss in kinetic energy is given
by the relation,
. .
K E
T
( )
( ) ( )
m m
m m u u e
2
1
1 2
1 2
1 2
2 2
=
+
− −
SOL 2.12 Option (A) is correct.
First of all we resolve all the force which are acting on the block.
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Given : PQ s
= where N = Normal fraction force
μ tan
< θ
Now from Newton’s second law,
F ma
=
sin
mg N
θ μ
− ma
= Acceleration of block
a =
sin cos
mg mg
θ μ θ
− ma
= cos
N mg θ
=
sin cos
g g
θ μ θ
− a
=
a cos
cos
sin
g θ
θ
θ μ
= −
: D ( )
cos tan
g θ θ μ
= − ...(i)
From the Newton;s second law of Motion,
s ut at
2
1 2
= + ( )
cos tan
g t
0
2
1 2
θ θ μ
= + − u 0
=
t
( )
cos tan
g
s
2
θ θ μ
=
−
SOL 2.13 Option (B) is correct.
If a system of forces acting on a body or system of bodies be in equilibrium
and the system has to undergo a small displacement consistent with the
geometrical conditions, then the algebraic sum of the virtual works done by
all the forces of the system is zero and total potential energy with respect to
each of the independent variable must be equal to zero.
SOL 2.14 Option (A) is correct.
First we solve this problem from Lami’s theorem. Here three forces are
given. Now we have to find the angle between these forces
Applying Lami’s theorem, we have
sin
F
90c sin sin
T T
120 150
AB AC
c c
= =
1
600
/ /
T T
3 2 1 2
AB AC
= =
TAB 600 300 520 N
2
3 3 .
#
= =
TAC 300 N
2
600
= =
20. PAGE 90 ENGINEERING MECHANICS CHAP 2
GATE Previous Year Solved Paper For Mechanical Engineering
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Alternative :
Now we using the Resolution of forces.
Resolve the TAB & TAC in x & y direction (horizontal & vertical components)
We use the Resolution of forces in x & y direction
0
Fx
Σ = , cos
T 60
AB c cos
T 30
AC c
=
T
T
AC
AB
2
3
1
2 3
#
= = ...(i)
0
Fy
Σ = , sin sin
T T
60 30
AB AC
c c
+ 600 N
=
T T
2
3
2
1
AB AC
+ N
600
=
T T
3 AB AC
+ 1200 N
= T T
3
AC
AB
= From equation (i)
Now, T T
3
3
AB
AB
+ 1200 N
=
T
4 AB 1200 3
=
TAB 520 N
4
1200 3
= =
and TAC 300 N
T
3 3
520
AB
= = =
SOL 2.15 Option (D) is correct.
Given ; x t t t
2 2
3 2
= + +
We know that,
v
dt
dx
= ( )
dt
d t t t
2 2
3 2
= + + t t
6 2 2
2
= + + ...(i)
We have to find the velocity & acceleration of particle, when motion stared,
So at t 0
= , v 2
=
Again differentiate equation (i) w.r.t. t
a 12 2
dt
dv
dt
d x t
2
2
= = = +
At t 0
= , a 2
=
21. CHAP 2 ENGINEERING MECHANICS PAGE 91
GATE Previous Year Solved Paper For Mechanical Engineering
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SOL 2.16 Option (A) is correct.
We have to make the diagram of simple pendulum
Here, We can see easily from the figure that tension in the string is balanced
by the weight of the bob and net force at the mean position is always zero.
SOL 2.17 Option (D) is correct.
Given : m m
1 2
= 1 kg
= , μ .
0 3
=
The FBD of the system is shown below :
For Book (1) 0
Fy
Σ = RN1 mg
= ...(i)
Then, Friction Force FN1 R mg
N1
μ μ
= =
From FBD of book second,
0
Fx
Σ = , F R R
N N
1 2
μ μ
= +
0
Fy
Σ = , RN2 2 mg
R mg mg mg
N1
= + = + = ...(ii)
For slip occurs between the books when
F R R
N N
1 2
$ μ μ
+ 2 mg
mg
$ μ μ #
+
F (3 )
mg
$ μ . ( . )
0 3 3 1 9 8
# #
$ .
8 82
$
It means the value of F is always greater or equal to the 8.82, for which slip
22. PAGE 92 ENGINEERING MECHANICS CHAP 2
GATE Previous Year Solved Paper For Mechanical Engineering
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occurs between two books.
So, F 8.83 N
=
SOL 2.18 Option (C) is correct.
Given : ω 2 /sec
rad
= , r 2 m
=
Tangential velocity of barrel, Vt rω
= 2 2
#
= 4 /sec
m
=
V V V
i j
r t
= + 3 4
i j
= +
Resultant velocity of shell, V ( ) ( )
3 4
2 2
= + 5 /sec
m
25
= =
SOL 2.19 Option (C) is correct.
Given : Mass of cage & counter weight = m kg each
Peak speed V
=
Initial velocity of both the cage and counter weight.
V1 /sec
m
V
=
Final velocity of both objects
V2 0
=
Initial kinetic Energy, E1 mV mV mV
2
1
2
1
2 2 2
= + =
Final kinetic Energy E2 ( ) ( )
m m
2
1 0
2
1 0 0
2 2
= + =
Now, Power = Rate of change of K.E.
t
E E
1 2
= −
t
mV2
=
SOL 2.20 Option (B) is correct.
Given : m1 1 kg
= , 10 /sec
m
V1 = , m2 20 kg
= , V2 = Velocity after striking
the wheel 1
r = meter
Applying the principal of linear momentum on the system
dt
dP 0
= P
& = constant
Initial Momentum = Final Momentum
m V
1 1
# ( )
m m V
1 2 2
= +
V2
( )
m m
m V
1 20
1 10
21
10
1 2
1 1 #
=
+
=
+
=
23. CHAP 2 ENGINEERING MECHANICS PAGE 93
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Now after the collision the wheel rolling with angular velocity ω.
So, V2 rω
= & ω 0.476
r
V
21 1
10
2
#
= = =
It is nearly equal to /
1 3.
SOL 2.21 Option (A) is correct.
First of all we consider all the forces, which are acting at point L.
Now sum all the forces which are acting along x direction,
FLK FLM
= Both are acting in opposite direction
Also summation of all the forces, which are acting along y-direction.
FLN 0
= Only one forces acting in y-direction
So the member LN is subjected to zero load.
SOL 2.22 Option (A) is correct.
Given : 981 10
k 3
#
= N/m, x 100
i = mm=0.1 m, m 100
= kg
Let, when mass m 100
= kg is put on the spring then spring compressed by
x mm. From the conservation of energy :
Energy stored in free state = Energy stored after the mass is attach.
( . .)
K E i ( . .) ( . .)
K E P E
f f
= +
kx
2
1
i
2
( 0.1)
kx mg x
2
1 2
= + +
kxi
2
2 ( 0.1)
kx mg x
2
= + +
Substitute the values, we get
( . )
981 10 0 1
3 2
# # (981 10 ) [2 100 9.81 ( 0.1)]
x x
3 2
# # # # #
= + +
10 10
3 2
#
−
( . )
x x
10 2 0 1
3 2
= + +
10 .
x x
1000 2 0 2
2
= + +
.
x x
1000 2 9 8
2
+ − 0
=
Solving above equation, we get
x
( ) ( . )
2 1000
2 2 4 1000 9 8
2
#
! #
=
− − −
2000
2 4 39200
2000
2 198
! !
= − + = −
On taking -ve sign, we get
24. PAGE 94 ENGINEERING MECHANICS CHAP 2
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x
2000
2 198
10
1
= − − =− , 100 mm
m =−
(-ve sign shows the compression of the spring)
SOL 2.23 Option (B) is correct.
Given : First Mass, m1 10 kg
=
Balancing Mass, m2 kg
20
=
We know the mass moment of inertia, I mk2
=
Where, k = Radius of gyration
Case (I) : When mass of 10 kg is rotates with uniform angular velocity ‘ω’
I1 m k
1 1
2
= 10 (0.2)2
#
= 10 0.04 0.4 kg m2
#
= = 0.2 m
k1 =
Case (II) : When balancing mass of 20 kg is attached then moment of inertia
I2 ( . ) ( . )
10 0 2 20 0 1
2 2
# #
= + . . .
0 4 0 2 0 6
= + = Here 0.2 m
k1 =
and 0.1 m
k2 =
Percent increase in mass moment of inertia,
I 100
.
. . 100
I
I I
0 4
0 6 0 4
1
2 1
# #
= − = − 100 50%
2
1
#
= =
SOL 2.24 Option (D) is correct.
Given : Weight of object W 2000 N
=
Coefficient of Friction μ 0.1
=
First of all we have to make the FBD of the system.
Here, RN = Normal reaction force acting by the pin joint.
F RN
μ
= = Friction force
In equilibrium condition of all the forces which are acting in y direction.
R R
N N
μ μ
+ 2000 N
=
RN
μ 1000 N
=
RN
.
10000 N
0 1
1000
= = .
0 1
μ =
Taking the moment about the pin, we get
10000 150
# F 300
#
=
F 5000 N
=
25. CHAP 2 ENGINEERING MECHANICS PAGE 95
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SOL 2.25 Option (A) is correct.
Given : AC CD DB EF CE DF l
= = = = = =
At the member EF uniform distributed load is acting, the U.D.L. is given
as “p” per unit length.
So, the total load acting on the element EF of length l
= Lord per unit length # Total length of element
p l pl
#
= =
This force acting at the mid point of EF . From the FBD we get that at A
and B reactions are acting because of the roller supports, in the upward
direction. In equilibrium condition,
Upward force = Downward forces
R R
a b
+ pl
= ...(i)
And take the moment about point A,
pl l l
2
# +
b l ( )
R l l l
b
= + +
pl l
2
3
# R l
3
b #
= & Rb
pl
2
=
Substitute the value of Rb in equation (i), we get
R
pl
2
a + pl
=
Ra pl
pl pl
2 2
= − = R
pl
2
b
= =
At point A we use the principal of resolution of forces in the y-direction,
F 0
y =
/ : sin
F 45
AE c R
pl
2
a
= =
FAE
sin
pl pl pl
2 45
1
2
2
2
c
# #
= = =
And FAC 45
cos
F
pl pl
2 2
1
2
AE c #
= = =
At C , No external force is acting. So,
FAC
pl
F
2 CD
= =
26. PAGE 96 ENGINEERING MECHANICS CHAP 2
GATE Previous Year Solved Paper For Mechanical Engineering
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SOL 2.26 Option (A) is correct.
Given : Mass of bullet m
=
Mass of block M
=
Velocity of bullet v
=
Coefficient of Kinematic friction = μ
Let, Velocity of system (Block + bullet) after striking the bullet u
=
We have to make the FBD of the box after the bullet strikes,
Friction Force (Retardation) Fr
=
Applying principal of conservation of linear momentum,
dt
dP 0
= or P mV
= .
tan
cons t
=
So, mv ( )
M m u
= +
u
M m
mv
=
+
...(i)
And, from the FBD the vertical force (reaction force),
RN ( )
M m g
= +
Fr ( )
R M m g
N
μ μ
= = +
Frictional retardation a
( )
( )
m M
F
M m
M m g
r μ
=
+
− =
+
− +
g
μ
=− ...(ii)
Negative sign show the retardation of the system (acceleration in opposite
direction). From the Newton’s third law of motion,
Vf
2
2
u as
2
= +
Vf = Final velocity of system (block + bullet) = 0
2
u as
2
+ 0
=
u2
as
2
=− ( )
g s
2 # #
μ
=− − gs
2μ
= From equation (ii)
Substitute the value of u from equation (i), we get
M m
mv 2
+
a k gs
2μ
=
( )
M m
m v
2
2 2
+
gs
2μ
=
v2 ( )
m
gs M m
2
2
2
μ
=
+
27. CHAP 2 ENGINEERING MECHANICS PAGE 97
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v gs
m
M m
2 #
μ
= +
b l m
M m gs
2μ
= +
SOL 2.27 Option (A) is correct.
Given : Mass of real m
=
Radius of gyration k
=
We have to make FBD of the system,
Where, T =Tension in the thread
mg = Weight of the system
Real is rolling down. So Angular acceleration ( )
α comes in the action
From FBD, For vertical translation motion,
mg T
− ma
= ...(i)
and for rotational motion,
MG
Σ IG α
=
T r
# mk
r
a
2
#
= I mk
G
2
= , /
a r
α =
T
r
mk a
2
2
#
= ...(ii)
From equation (i) & (ii) Substitute the value of T in equation (i), we get
mg
r
mk a
2
2
#
− ma
=
mg a
r
mk m
2
2
= +
; E
a
k r
gr
2 2
2
=
+
...(iii)
SOL 2.28 Option (C) is correct.
From previous question, T mg ma
= −
Substitute the value of a from equation (iii), we get
T
( )
mg m
k r
gr
2 2
2
#
= −
+ ( )
( )
k r
mg k r mgr
2 2
2 2 2
=
+
+ −
k r
mgk
2 2
2
=
+
28. PAGE 98 ENGINEERING MECHANICS CHAP 2
GATE Previous Year Solved Paper For Mechanical Engineering
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SOL 2.29 Option (D) is correct.
We know that a particle requires the velocity of 11.2 /
km s for escape it from
the earth’s gravitational field. The angle α does not effect on it.
SOL 2.30 Option (C) is correct.
The BD is the diagonal of the square ABCD and CBD 45c
= .
From the BCE
T sin45c
BC
CE
= & CE 1 45
sin
2
1
c
#
= = unit
where CE is the height of the triangle BCD
T .
Now, the area moment of inertia of a triangle about its base BD is bh
12
3
where b = base of triangle & h = height of triangle
So, the triangle ABD
T are same and required moment of inertia of the
square ABCD about its diagonal is,
I 1 ( ) ( )
BD CE
2
12
3
# # #
=
6
1 2
2
1
12
1
3
# #
= =
c m unit
SOL 2.31 Option (A) is correct.
The reactions at the hinged support will be in only vertical direction as
external loads are vertical.
Now, consider the FBD of entire truss. In equilibrium of forces.
R R
a f
+ 1 1 2 kN
= + = ...(i)
Taking moment about point A, we get
R L
3
f # 1 1 2 3
L L L
# #
= + =
Rf 1 kN
=
From equation (i), Ra 2 1 1 kN
= − =
29. CHAP 2 ENGINEERING MECHANICS PAGE 99
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First consider the FBD of joint A with the direction of forces assumed in
the figure.
Resolving force vertically, we get
Ra sin
F 45
AB c
=
FAB
sin
kN
45
1 2
c
= = (Compression)
Resolving forces horizontally
FAC cos
F 45
AB c 1 kN
2
2
1
#
= = (Tension)
Consider the FBD of joint B with known value of force FAB in member AB
Resolving forces vertically,
FBC cos
F 45
AB c
= 1 kN
2
2
1
#
= = (Tension)
Resolving forces horizontally,
FBD sin
F 45
AB c
= 1 kN
2
2
1
#
= = (Compression)
Consider the FBD of joint C with known value of force FBC and FAC
Resolving forces vertically,
1 sin
F F 45
BC CD c
= +
30.
31.
32.
33.
34. PAGE 104 ENGINEERING MECHANICS CHAP 2
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1 sin
F F
1 45 0
CD CD
&
c
= + =
SOL 2.32 Option (D) is correct.
From the FBD of the system.
RN cos
mg 45c
=
All surfaces are smooth, so there is no frictional force at the surfaces.
The downward force sin
mg 45c is balanced by cos
P 45c.
sin
mg 45c cos
P 45c
=
mg
2
1
# P
2
1
#
= & P mg
=
SOL 2.33 Option (C) is correct.
In this case the motion of mass m is only in x -direction. So, the linear
momentum is only in x -direction & it remains conserved.
Also from Energy conservation law the energy remains constant i.e. energy
is also conserved.
**********